CN210338267U - Unmanned aerial vehicle of pneumatic overall arrangement - Google Patents
Unmanned aerial vehicle of pneumatic overall arrangement Download PDFInfo
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- CN210338267U CN210338267U CN201920925188.9U CN201920925188U CN210338267U CN 210338267 U CN210338267 U CN 210338267U CN 201920925188 U CN201920925188 U CN 201920925188U CN 210338267 U CN210338267 U CN 210338267U
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Abstract
The utility model discloses an unmanned aerial vehicle of pneumatic overall arrangement, which comprises a main frame, first slide rail has been seted up in the left side of body frame bottom, the first motor of right-hand member fixedly connected with of first slide rail, the inboard left end of first slide rail is rotated and is connected with first pivot, the first guide arm of right-hand member fixedly connected with of first pivot, just first guide arm with first motor is connected, the surface threaded connection of first guide arm has first slider, just first slider with first slide rail is identical, the first backup pad of bottom fixedly connected with of first slider, the both ends fixedly connected with second motor of first backup pad side. This unmanned aerial vehicle of aerodynamic layout, the position of first wing is adjusted through first motor, the angle of first wing is adjusted through the second motor, the position of second wing is adjusted through the third motor, the angle of second wing is adjusted through the fourth motor, is convenient for change the air current of flying.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle field specifically is an unmanned aerial vehicle of pneumatic overall arrangement.
Background
An unmanned aircraft is an unmanned aircraft that is operated using a radio remote control device and self-contained program control means, or is operated autonomously, either completely or intermittently, by an on-board computer.
Present unmanned aerial vehicle can not adjust when flying, because highly different, the air current of formation also can be different, can cause the damage to unmanned aerial vehicle when flying, reduces its life, and is unfavorable for flight and control, for this reason, we propose the unmanned aerial vehicle of a pneumatic overall arrangement.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle of pneumatic overall arrangement has solved the problem that proposes in the background art.
In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle with pneumatic layout comprises a main frame, wherein a first sliding rail is arranged on the left side of the bottom of the main frame, a first motor is fixedly connected to the right end of the first sliding rail, a first rotating shaft is rotatably connected to the left end of the inner side of the first sliding rail, a first guide rod is fixedly connected to the right end of the first rotating shaft and connected with the first motor, a first sliding block is connected to the outer surface of the first guide rod in a threaded manner and is matched with the first sliding rail, a first supporting plate is fixedly connected to the bottom of the first sliding block, a second motor is fixedly connected to the two ends of the side surface of the first supporting plate, a first connecting plate is rotatably connected to the two ends of the first supporting plate through a second rotating shaft, a first wing is fixedly connected to the other end of the first connecting plate, a second sliding rail is arranged on the right side of the bottom of the main frame, the left end fixedly connected with third motor of second slide rail, the inboard right-hand member of second slide rail rotates and is connected with the third pivot, the left end fixedly connected with second guide arm of third pivot, just the second guide arm with the third motor is connected, the surface threaded connection of second guide arm has the second slider, just the second slider with the second slide rail is identical, the bottom fixedly connected with second backup pad of second slider, the both ends fixedly connected with fourth motor of second backup pad side, the both ends of second backup pad are rotated through the fourth pivot and are connected with the second connecting plate, just the fourth motor with the fourth pivot is connected, the other end fixedly connected with second wing of second connecting plate.
As a preferred embodiment of the present invention, the left end of the main frame is rotatably connected with the propeller, and the middle of the upper surface of the main frame is fixedly connected with the protection box.
As a preferred embodiment of the present invention, the bottom of the protection box is fixedly connected with a battery, and the bottom of the side of the battery is fixedly connected with a charging hole.
As a preferred embodiment of the present invention, the controller is fixedly connected to the upper portion of the protection box, and the first motor, the second motor, the third motor and the fourth motor are all connected to the controller through wires.
As a preferred embodiment of the present invention, the first wing and the second wing are both provided with two wings, and are symmetrically disposed.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the utility model discloses an unmanned aerial vehicle of pneumatic overall arrangement, start first motor through the controller, first motor drives first guide arm and rotates, first guide arm drives first slider and moves, first slider drives first backup pad and moves, first backup pad drives first wing and moves, the position of the first wing of convenient regulation, be convenient for change the air current of flying, start second motor through the controller, the second motor drives the second pivot and rotates, the second pivot drives first connecting plate and rotates, first connecting plate drives first wing and rotates, thereby be convenient for adjust the angle of first wing, be convenient for change the air current of flying;
2. the utility model discloses an unmanned aerial vehicle of pneumatic overall arrangement, start the third motor through the controller, the third motor drives the second guide arm and rotates, the second guide arm drives the second slider and moves, the second slider drives the second backup pad and moves, the second backup pad drives the second wing and moves, be convenient for adjust the position of second wing, be convenient for change the air current of flying, start the fourth motor through the controller, the fourth motor drives the fourth pivot and rotates, the fourth pivot drives the second connecting plate and rotates, the second connecting plate drives the second wing and rotates, thereby be convenient for adjust the angle of second wing, be convenient for change the air current of flying;
3. the utility model discloses an unmanned aerial vehicle of pneumatic overall arrangement provides the power through the battery for the device, charges for the battery through the hole that charges, plays the guard action to controller and battery through the guard box, and the screw that is equipped with through the body frame front end plays the auxiliary action, and this novel operation of being convenient for is comparatively practical, is fit for extensively promoting and using.
Drawings
Other features, objects and advantages of the invention will become more apparent upon reading of the detailed description of non-limiting embodiments with reference to the following drawings:
fig. 1 is a front view of an unmanned aerial vehicle of a pneumatic layout of the present invention;
figure 2 is the utility model relates to an unmanned aerial vehicle of pneumatic overall arrangement look sideways at enlarged cross-sectional view.
In the figure: the main frame 1, the screw 11, the guard box 2, the battery 21, the hole 22 that charges, the controller 23, first slide rail 3, first motor 31, first pivot 32, first guide arm 33, first slider 34, first backup pad 4, second motor 41, second pivot 42, first connecting plate 43, first wing 44, second slide rail 5, third motor 51, third pivot 52, second guide arm 53, second slider 54, second backup pad 6, fourth motor 61, fourth pivot 62, second connecting plate 63, second wing 64.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.
In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.
Referring to fig. 1-2, the present invention provides a technical solution: an unmanned aerial vehicle with a pneumatic layout comprises a main frame 1, wherein a first slide rail 3 is arranged on the left side of the bottom of the main frame 1, a first motor 31 is fixedly connected to the right end of the first slide rail 3, a first rotating shaft 32 is rotatably connected to the left end of the inner side of the first slide rail 3, a first guide rod 33 is fixedly connected to the right end of the first rotating shaft 32, the first guide rod 33 is connected with the first motor 31, a first sliding block 34 is connected to the outer surface of the first guide rod 33 in a threaded manner, the first sliding block 34 is matched with the first slide rail 3, a first supporting plate 4 is fixedly connected to the bottom of the first sliding block 34, a second motor 41 is fixedly connected to the two ends of the side surface of the first supporting plate 4, a first connecting plate 43 is rotatably connected to the two ends of the first supporting plate 4 through a second rotating shaft 42, and the second motor 41 is connected with the second rotating shaft 42, the other end of the first connecting plate 43 is fixedly connected with a first wing 44, the right side of the bottom of the main frame 1 is provided with a second slide rail 5, the left end of the second slide rail 5 is fixedly connected with a third motor 51, the right end of the inner side of the second slide rail 5 is rotatably connected with a third rotating shaft 52, the left end of the third rotating shaft 52 is fixedly connected with a second guide rod 53, the second guide rod 53 is connected with the third motor 51, the outer surface of the second guide rod 53 is in threaded connection with a second slide block 54, the second slide block 54 is matched with the second slide rail 5, the bottom of the second slide block 54 is fixedly connected with a second supporting plate 6, the two ends of the side surface of the second supporting plate 6 are fixedly connected with a fourth motor 61, the two ends of the second supporting plate 6 are rotatably connected with a second connecting plate 63 through a fourth rotating shaft 62, and the fourth motor 61 is connected with the fourth rotating shaft 62, the other end of the second connecting plate 63 is fixedly connected with a second wing 64, in this embodiment (as shown in fig. 1 and fig. 2), the controller 23 is used to start the first motor 31, the first motor 31 drives the first guide rod 33 to rotate, the first guide rod 33 drives the first sliding block 34 to move, the first sliding block 34 drives the first supporting plate 4 to move, the first supporting plate 4 drives the first wing 44 to move, so as to adjust the position of the first wing 44, so as to change the flying airflow, the controller 23 is used to start the second motor 41, the second motor 41 drives the second rotating shaft 42 to rotate, the second rotating shaft 42 drives the first connecting plate 43 to rotate, the first connecting plate 43 drives the first wing 44 to rotate, so as to adjust the angle of the first wing 44, so as to change the flying airflow, the controller 23 is used to start the third motor 51, the third motor 51 drives the second guide rod 53 to rotate, the second guide rod 53 drives the second sliding block 54 to move, the second sliding block 54 drives the second supporting plate 6 to move, the second supporting plate 6 drives the second wing 64 to move, the position of the second wing 64 is convenient to adjust, the flying airflow is convenient to change, the fourth motor 61 is started through the controller 23, the fourth motor 61 drives the fourth rotating shaft 62 to rotate, the fourth rotating shaft 62 drives the second connecting plate 63 to rotate, the second connecting plate 63 drives the second wing 64 to rotate, the angle of the second wing 64 is convenient to adjust, the flying airflow is convenient to change, a power supply is provided for the device through the battery 21, the battery 21 is charged through the charging hole 22, the controller 23 and the battery 21 are protected through the protection box 2, and the auxiliary effect is achieved through the propeller 11 arranged at the front end of the main frame 1.
Referring to fig. 1-2, a propeller 11 is rotatably connected to the left end of the main frame 1, and a protection box 2 is fixedly connected to the middle of the upper surface of the main frame 1, and plays an auxiliary role through the propeller 11.
Referring to fig. 2, a battery 21 is fixedly connected to the bottom of the protection box 2, a charging hole 22 is fixedly connected to the bottom of the side surface of the battery 21, and the battery 21 is charged through the charging hole 22.
Referring to fig. 2, a controller 23 is fixedly connected to an upper portion inside the protection box 2, and the first motor 31, the second motor 41, the third motor 51 and the fourth motor 61 are all connected to the controller 23 through wires, and are controlled by the controller 23.
Referring to fig. 1, two first wings 44 and two second wings 64 are symmetrically disposed, and assist in flying through the first wings 44 and the second wings 64.
The working principle is as follows: it should be noted that the present invention is an unmanned aerial vehicle with a pneumatic layout, which includes a main frame 1, a propeller 11, a protection box 2, a battery 21, a charging hole 22, a controller 23, a first slide rail 3, a first motor 31, a first rotating shaft 32, a first guide rod 33, a first slider 34, a first support plate 4, a second motor 41, a second rotating shaft 42, a first connecting plate 43, a first wing 44, a second slide rail 5, a third motor 51, a third rotating shaft 52, a second guide rod 53, a second slider 54, a second support plate 6, a fourth motor 61, a fourth rotating shaft 62, a second connecting plate 63, a second wing 64, and all components are universal standard components or components known by technicians in the art, and the structure and principle of the present invention can be known by technicians or by conventional experimental methods, when in use, a user starts the first motor 31 through the controller 23, the first motor 31 drives the first guide rod 33 to rotate, the first guide rod 33 drives the first sliding block 34 to move, the first sliding block 34 drives the first support plate 4 to move, the first support plate 4 drives the first wing 44 to move, so as to adjust the position of the first wing 44 and change the flying air flow conveniently, the controller 23 is used for starting the second motor 41, the second motor 41 drives the second rotating shaft 42 to rotate, the second rotating shaft 42 drives the first connecting plate 43 to rotate, the first connecting plate 43 drives the first wing 44 to rotate, so as to adjust the angle of the first wing 44 and change the flying air flow conveniently, the controller 23 is used for starting the third motor 51, the third motor 51 drives the second guide rod 53 to rotate, the second guide rod 53 drives the second sliding block 54 to move, the second sliding block 54 drives the second support plate 6 to move, the second support plate 6 drives the second wing 64 to move, so as to adjust the position of the second wing 64, be convenient for change the air current of flying, start fourth motor 61 through controller 23, fourth motor 61 drives fourth pivot 62 and rotates, fourth pivot 62 drives second connecting plate 63 and rotates, second connecting plate 63 drives second wing 64 and rotates, thereby be convenient for adjust the angle of second wing 64, be convenient for change the air current of flying, provide the power for the device through battery 21, charge for battery 21 through charging hole 22, play the guard action to controller 23 and battery 21 through guard box 2, screw 11 through being equipped with of body frame 1 front end, play the additional action.
The basic principles and the main features of the invention and the advantages of the invention have been shown and described above, it will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, but that the invention may be embodied in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.
Claims (5)
1. The utility model provides an unmanned aerial vehicle of pneumatic overall arrangement, includes body frame (1), its characterized in that: the left side of the bottom of the main frame (1) is provided with a first sliding rail (3), the right end of the first sliding rail (3) is fixedly connected with a first motor (31), the left end of the inner side of the first sliding rail (3) is rotatably connected with a first rotating shaft (32), the right end of the first rotating shaft (32) is fixedly connected with a first guide rod (33), the first guide rod (33) is connected with the first motor (31), the outer surface of the first guide rod (33) is in threaded connection with a first sliding block (34), the first sliding block (34) is matched with the first sliding rail (3), the bottom of the first sliding block (34) is fixedly connected with a first supporting plate (4), the two ends of the side surface of the first supporting plate (4) are fixedly connected with a second motor (41), the two ends of the first supporting plate (4) are rotatably connected with a first connecting plate (43) through a second rotating shaft (42), the second motor (41) is connected with the second rotating shaft (42), the other end of the first connecting plate (43) is fixedly connected with a first wing (44), the right side of the bottom of the main frame (1) is provided with a second sliding rail (5), the left end of the second sliding rail (5) is fixedly connected with a third motor (51), the right end of the inner side of the second sliding rail (5) is rotatably connected with a third rotating shaft (52), the left end of the third rotating shaft (52) is fixedly connected with a second guide rod (53), the second guide rod (53) is connected with the third motor (51), the outer surface of the second guide rod (53) is in threaded connection with a second sliding block (54), the second sliding block (54) is matched with the second sliding rail (5), the bottom of the second sliding block (54) is fixedly connected with a second supporting plate (6), and the two ends of the side surface of the second supporting plate (6) are fixedly connected with a fourth motor (61), the two ends of the second supporting plate (6) are rotatably connected with a second connecting plate (63) through a fourth rotating shaft (62), the fourth motor (61) is connected with the fourth rotating shaft (62), and the other end of the second connecting plate (63) is fixedly connected with a second wing (64).
2. A pneumatically arranged drone according to claim 1, characterized in that: the left end of the main frame (1) is rotatably connected with a propeller (11), and the middle of the upper surface of the main frame (1) is fixedly connected with a protection box (2).
3. A pneumatically arranged drone according to claim 2, characterized in that: the bottom fixedly connected with battery (21) of guard box (2), the bottom fixedly connected with hole of charging (22) of battery (21) side.
4. A pneumatically arranged drone according to claim 2, characterized in that: the upper portion inside the protection box (2) is fixedly connected with a controller (23), and the first motor (31), the second motor (41), the third motor (51) and the fourth motor (61) are connected with the controller (23) through wires.
5. A pneumatically arranged drone according to claim 1, characterized in that: the first wing (44) and the second wing (64) are arranged in two and are symmetrically arranged.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920925188.9U CN210338267U (en) | 2019-06-19 | 2019-06-19 | Unmanned aerial vehicle of pneumatic overall arrangement |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920925188.9U CN210338267U (en) | 2019-06-19 | 2019-06-19 | Unmanned aerial vehicle of pneumatic overall arrangement |
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| Publication Number | Publication Date |
|---|---|
| CN210338267U true CN210338267U (en) | 2020-04-17 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920925188.9U Active CN210338267U (en) | 2019-06-19 | 2019-06-19 | Unmanned aerial vehicle of pneumatic overall arrangement |
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| Country | Link |
|---|---|
| CN (1) | CN210338267U (en) |
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- 2019-06-19 CN CN201920925188.9U patent/CN210338267U/en active Active
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